Combustion chamber for gas turbine engines
US4062182A · kind A · utility
24Cited by
10References
4Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 15, 1975 |
| Grant date | Dec 13, 1977 |
| Priority date | — |
| Expiry date | Dec 15, 1995 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02E20/34
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A combustion engine for gas turbine engines, constituted of an outer housing and having at least one flame tube inserted therein which is suppliable with secondary or mixing air through the intermediary of an annular passageway formed between the outer housing and the flame tube while, on the other side, the primary zone within the flame tube has fuel-enriched combustion air conveyable thereto, and wherein there are provided at least two fuel atomizer nozzles which are controllable independently of each other.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.